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CA2565147A1 - Method of monitoring gas turbine engine operation - Google Patents

Method of monitoring gas turbine engine operation Download PDF

Info

Publication number
CA2565147A1
CA2565147A1 CA002565147A CA2565147A CA2565147A1 CA 2565147 A1 CA2565147 A1 CA 2565147A1 CA 002565147 A CA002565147 A CA 002565147A CA 2565147 A CA2565147 A CA 2565147A CA 2565147 A1 CA2565147 A1 CA 2565147A1
Authority
CA
Canada
Prior art keywords
gas turbine
turbine engine
engine operation
monitoring gas
counter value
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CA002565147A
Other languages
French (fr)
Other versions
CA2565147C (en
Inventor
Mark Edward Feeney
Keith J. Leslie
Yusuf Razi Syed
Simon J. Hartropp
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Pratt and Whitney Canada Corp
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of CA2565147A1 publication Critical patent/CA2565147A1/en
Application granted granted Critical
Publication of CA2565147C publication Critical patent/CA2565147C/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D19/00Starting of machines or engines; Regulating, controlling, or safety means in connection therewith
    • GPHYSICS
    • G07CHECKING-DEVICES
    • G07CTIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
    • G07C5/00Registering or indicating the working of vehicles
    • G07C5/08Registering or indicating performance data other than driving, working, idle, or waiting time, with or without registering driving, working, idle or waiting time
    • G07C5/0816Indicating performance data, e.g. occurrence of a malfunction
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/50Application for auxiliary power units (APU's)
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/10Stators
    • F05D2240/12Fluid guiding means, e.g. vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/80Diagnostics
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/30Control parameters, e.g. input parameters
    • F05D2270/303Temperature
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/40Type of control system
    • F05D2270/44Type of control system active, predictive, or anticipative

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Testing Of Engines (AREA)

Abstract

A system, method and apparatus for monitoring the performance of a gas turbine engine. A counter value indicative of the comparison between the engine condition and the threshold condition is adjusted. The aircraft operator is warned of an impending maintenance condition based on the counter value and determines an appropriate course of action.
CA002565147A 2004-05-21 2005-05-20 Method of monitoring gas turbine engine operation Expired - Fee Related CA2565147C (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US10/850,436 2004-05-21
US10/850,436 US7487029B2 (en) 2004-05-21 2004-05-21 Method of monitoring gas turbine engine operation
PCT/CA2005/000774 WO2005114129A1 (en) 2004-05-21 2005-05-20 Method of monitoring gas turbine engine operation

Publications (2)

Publication Number Publication Date
CA2565147A1 true CA2565147A1 (en) 2005-12-01
CA2565147C CA2565147C (en) 2009-10-13

Family

ID=35376272

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002565147A Expired - Fee Related CA2565147C (en) 2004-05-21 2005-05-20 Method of monitoring gas turbine engine operation

Country Status (5)

Country Link
US (2) US7487029B2 (en)
EP (1) EP1747446A4 (en)
JP (1) JP2007538234A (en)
CA (1) CA2565147C (en)
WO (1) WO2005114129A1 (en)

Families Citing this family (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7487029B2 (en) * 2004-05-21 2009-02-03 Pratt & Whitney Canada Method of monitoring gas turbine engine operation
US7286923B2 (en) * 2005-09-30 2007-10-23 General Electric Company System and method for estimating turbine engine deterioration rate with noisy data
US7824147B2 (en) * 2006-05-16 2010-11-02 United Technologies Corporation Airfoil prognosis for turbine engines
US20080082230A1 (en) * 2006-10-02 2008-04-03 Harvey David F Process for estimating operational availability of a system
FR2923909B1 (en) * 2007-11-15 2009-11-27 Renault Sas DEVICE FOR GENERATING AN INFORMATION SIGNAL REPRESENTATIVE OF A WEAR RATE OF A MECHANICAL PART OF A MOTOR
GB0722398D0 (en) * 2007-11-15 2007-12-27 Rolls Royce Plc A method of monitoring a gas turbine engine
US20100318443A1 (en) * 2009-06-16 2010-12-16 Christopher Michael Culp Apparatus for assessing and method for delivering an equipment upgrade proposal
US20110106680A1 (en) * 2009-10-30 2011-05-05 General Electric Company Turbine operation degradation determination system and method
IT1401923B1 (en) * 2010-09-09 2013-08-28 Nuovo Pignone Spa METHODS AND DEVICES FOR TESTING A LOW-SPEED LOW-TIME ROTOR IN A TURBOMACCHINE
US8751423B2 (en) 2010-11-30 2014-06-10 General Electric Company Turbine performance diagnostic system and methods
US8494889B2 (en) * 2011-06-14 2013-07-23 International Business Machines Corporation Optimized maintenance schedules based on smart city maintenance profiles
CN102343983A (en) * 2011-07-07 2012-02-08 中国国际航空股份有限公司 Airplane APU (Auxiliary Power Unit) performance detecting method
CN102320382A (en) * 2011-07-07 2012-01-18 中国国际航空股份有限公司 Aircraft performance detection method
US9127597B2 (en) * 2011-09-23 2015-09-08 The Boeing Company Sensor system
FR2986506B1 (en) * 2012-02-06 2015-06-26 Eurocopter France METHOD AND DEVICE FOR REALIZING A HEALTH CONTROL OF A TURBOMOTEUR OF AN AIRCRAFT COMPRISING AT LEAST ONE TURBOMOTEUR
FR2986505B1 (en) * 2012-02-06 2015-06-26 Eurocopter France METHOD FOR OPTIMIZING PERFORMANCE OF AN AIRCRAFT, DEVICE AND AIRCRAFT
FR2986507B1 (en) 2012-02-06 2014-01-17 Eurocopter France METHOD AND DEVICE FOR REALIZING A HEALTH CONTROL OF A TURBOMOTEUR OF AN AIRCRAFT COMPRISING AT LEAST ONE TURBOMOTEUR
WO2014005070A1 (en) * 2012-06-28 2014-01-03 Alaska Airlines, Inc. Robust systems and methods for improving passenger jet aircraft fuel economy
EP2706422B1 (en) * 2012-09-11 2016-07-27 Siemens Aktiengesellschaft Method for computer-implemented monitoring of the operation of a technical system, in particular an electrical energy production assembly
FR2997451B1 (en) * 2012-10-26 2015-01-16 Snecma SYSTEM FOR MONITORING A SET OF ENGINE COMPONENTS
US9243970B2 (en) 2012-11-30 2016-01-26 Pratt & Whitney Canada Corp. Method and system for integrating gas turbine trim balancing system into electronic engine controls
FR2999227B1 (en) * 2012-12-10 2015-02-06 Snecma METHOD FOR BALANCING A TURBOMACHINE ROTOR AND BALANCED ROTOR BY SUCH A METHOD
US20140178175A1 (en) * 2012-12-21 2014-06-26 United Technologies Corporation Air turbine starter monitor system
CN105122633B (en) 2013-04-09 2019-04-05 热成像雷达有限责任公司 Step motor control system and method
EP2984640B1 (en) * 2013-04-09 2019-12-18 Thermal Imaging Radar, LLC Fire detection system
GB2513132B (en) 2013-04-16 2015-05-27 Ge Aviat Systems Ltd Method for predicting a bleed air system fault
FR3007459B1 (en) * 2013-06-19 2016-10-14 Airbus Operations Sas SYSTEM AND METHOD FOR ROTATING A ROTARY MEMBER OF A MECHANICAL DEVICE, IN PARTICULAR A TURBOMACHINE.
CN104343476B (en) * 2013-07-24 2016-06-08 中国国际航空股份有限公司 Airplane auxiliary power unit turbine efficiency monitoring method and apparatus
BR112016002720B1 (en) 2013-08-09 2021-11-23 Thermal Imaging Radar, LLC LOCAL SYSTEM AND METHOD FOR ANALYZING AND CLASSIFYING INDIVIDUAL IMAGE FRAMES OF PANORAMIC IMAGE DATA
DE102013110151A1 (en) * 2013-09-16 2015-04-02 Airbus Defence and Space GmbH A method of detecting an error in an array, detection device and missile
FR3014952B1 (en) * 2013-12-13 2016-01-22 Snecma PREDICTION OF MAINTENANCE OPERATIONS TO BE APPLIED TO A MOTOR
FR3024434B1 (en) * 2014-07-29 2016-08-05 Airbus Helicopters METHOD AND DEVICE FOR DETECTING THE ENHANCEMENT OF AN AIR INLET OF A TURBOMOTEUR
WO2016053841A1 (en) 2014-09-29 2016-04-07 Laird Technologies, Inc. Telematics devices and methods for vehicle ignition detection
FR3028331B1 (en) * 2014-11-10 2016-12-30 Snecma METHOD FOR MONITORING AN AIRCRAFT ENGINE IN OPERATION IN A GIVEN ENVIRONMENT
EP3035140B1 (en) * 2014-12-19 2018-09-12 Rolls-Royce Deutschland Ltd & Co KG Equipment health monitoring method and system
MX368852B (en) 2015-03-31 2019-10-18 Thermal Imaging Radar Llc Setting different background model sensitivities by user defined regions and background filters.
JP6560920B2 (en) * 2015-07-14 2019-08-14 日本光電工業株式会社 Blood pressure measurement device
US10099804B2 (en) 2016-06-16 2018-10-16 General Electric Company Environmental impact assessment system
US9976907B1 (en) 2017-07-05 2018-05-22 The Boeing Company Airplane-mounted external fire detection system
US10574886B2 (en) 2017-11-02 2020-02-25 Thermal Imaging Radar, LLC Generating panoramic video for video management systems
FR3094350B1 (en) * 2019-04-01 2021-03-12 Safran Aircraft Engines Method for monitoring at least one aircraft engine
FR3101669B1 (en) * 2019-10-07 2022-04-08 Safran Aircraft engine tracking computer device, method and program
US11601605B2 (en) 2019-11-22 2023-03-07 Thermal Imaging Radar, LLC Thermal imaging camera device
CN111862388B (en) * 2020-07-17 2021-09-07 南京航空航天大学 Data-based calculation method for exhaust temperature margin life of aircraft engine
US20230339620A1 (en) * 2022-04-22 2023-10-26 Pratt & Whitney Canada Corp. Operating aircraft propulsion system during engine-inoperative event

Family Cites Families (76)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE318194B (en) * 1968-06-24 1969-12-01 Saab Ab
GB1327031A (en) 1969-10-21 1973-08-15 Secr Defence Take-off velocity monitor for aircraft
US3871444A (en) * 1971-08-02 1975-03-18 Beckman Instruments Inc Water quality analysis system with multicircuit single shell heat exchanger
US3880226A (en) * 1971-08-02 1975-04-29 Edwin A Houser Water quality analysis system with multicircuit single shell heat exchanger
US3762667A (en) * 1971-12-29 1973-10-02 D Pender Vertical take-off and landing aircraft
US3851464A (en) 1973-08-28 1974-12-03 Gen Motors Corp Gas turbine fuel control
US4028884A (en) * 1974-12-27 1977-06-14 Westinghouse Electric Corporation Control apparatus for controlling the operation of a gas turbine inlet guide vane assembly and heat recovery steam generator for a steam turbine employed in a combined cycle electric power generating plant
US4046003A (en) * 1976-05-07 1977-09-06 United Technologies Corporation Engine turbocharger diagnostics
US4215412A (en) * 1978-07-13 1980-07-29 The Boeing Company Real time performance monitoring of gas turbine engines
US4428199A (en) * 1979-02-28 1984-01-31 Semco Instruments, Inc. Turbocharger control system
US4402561A (en) * 1981-03-27 1983-09-06 Amp Incorporated Socket for integrated circuit package with extended leads
US4787053A (en) * 1981-12-30 1988-11-22 Semco Instruments, Inc. Comprehensive engine monitor and recorder
US4500966A (en) * 1982-05-26 1985-02-19 Chandler Evans Inc. Super contingency aircraft engine control
JPS593335A (en) * 1982-06-30 1984-01-10 Hitachi Ltd Method for maintenance and monitor of gas turbine plant
US4590562A (en) * 1982-12-28 1986-05-20 United Technologies Corporation Statistically correlated electrostatic engine diagnostics
US4904999A (en) 1983-03-28 1990-02-27 The Boeing Company Fault monitoring system for aircraft power control units
US4583360A (en) 1983-03-31 1986-04-22 Dresser Industries, Inc. Electronic fuel control system for gas turbine
US4798515A (en) * 1986-05-19 1989-01-17 The United States Of America As Represented By The Secretary Of The Air Force Variable nozzle area turbine vane cooling
US4783957A (en) * 1986-12-23 1988-11-15 Sundstrand Corporation Fuel control circuit for a turbine engine
US5047942A (en) 1987-08-06 1991-09-10 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Airplane takeoff and landing performance monitoring system
US4928240A (en) * 1988-02-24 1990-05-22 General Electric Company Active clearance control
GB2225125A (en) 1988-11-16 1990-05-23 Sundstrand Corp Turbine monitoring system
GB8902645D0 (en) 1989-02-07 1989-03-30 Smiths Industries Plc Monitoring
US5018069A (en) 1989-07-13 1991-05-21 Howell Instruments, Inc. Reference system and method for diagnosing aircraft engine conditions
US5610815A (en) * 1989-12-11 1997-03-11 Caterpillar Inc. Integrated vehicle positioning and navigation system, apparatus and method
US5375059A (en) * 1990-02-05 1994-12-20 Caterpillar Inc. Vehicle position determination system and method
WO1993018494A1 (en) 1992-03-11 1993-09-16 The Boeing Company Thermal condition sensor system for monitoring equipment operation
US5437539A (en) * 1992-07-22 1995-08-01 Massachusetts Institute Of Technology Apparatus for the dynamic control of rotating stall and surge in turbo machines and the like
EP0636955B1 (en) * 1993-07-26 1998-11-04 Hitachi, Ltd. Control unit for vehicle and total control system therefor
US5479350A (en) 1993-08-23 1995-12-26 B&D Instruments And Avionics, Inc. Exhaust gas temperature indicator for a gas turbine engine
US5726891A (en) * 1994-01-26 1998-03-10 Sisson; Patterson B. Surge detection system using engine signature
US5487265A (en) * 1994-05-02 1996-01-30 General Electric Company Gas turbine coordinated fuel-air control method and apparatus therefor
US5485833A (en) * 1994-06-10 1996-01-23 Dietz; Henry G. Breath exposure synchronizer
JP2655095B2 (en) * 1994-08-25 1997-09-17 日本電気株式会社 Flight plan evaluation generation device mounted on aircraft
US5488833A (en) 1994-09-26 1996-02-06 Stewart; Jeffrey Tangential flow cold trap
US6199372B1 (en) * 1996-04-26 2001-03-13 Komatsu Ltd. Apparatus and method for regenerating NOx catalyst for diesel engine
JP3248428B2 (en) * 1996-06-18 2002-01-21 ヤマハ株式会社 Electronic device and channel control method for data transmission system
EP1010114A1 (en) 1996-11-27 2000-06-21 Sundstrand Corporation, Inc. Method of maintaining components subject to fatigue failure
US5919267A (en) 1997-04-09 1999-07-06 Mcdonnell Douglas Corporation Neural network fault diagnostics systems and related method
US6112141A (en) * 1997-10-15 2000-08-29 Dassault Aviation Apparatus and method for graphically oriented aircraft display and control
JP3681033B2 (en) * 1997-11-17 2005-08-10 株式会社小松製作所 Life prediction apparatus for machine having engine and heat source
JPH11325293A (en) * 1998-05-15 1999-11-26 Fujikoki Corp Pressure regulating valve for variable displacement compressor
US6341238B1 (en) * 1998-10-01 2002-01-22 United Technologies Corporation Robust engine variable vane monitor logic
US6202403B1 (en) 1998-12-22 2001-03-20 General Electric Company Core compartment valve cooling valve scheduling
JP2000257449A (en) * 1999-03-05 2000-09-19 Toshiba Corp Gas turbine system
US6164057A (en) * 1999-03-16 2000-12-26 General Electric Co. Gas turbine generator having reserve capacity controller
US6346892B1 (en) * 1999-05-07 2002-02-12 Honeywell International Inc. Method and apparatus for aircraft systems management
US6487478B1 (en) 1999-10-28 2002-11-26 General Electric Company On-board monitor for railroad locomotive
US6408259B1 (en) * 2000-02-01 2002-06-18 General Electric Company Alert generation for trend performance analysis
GB0011251D0 (en) * 2000-05-11 2000-06-28 Lucas Industries Ltd Fault monitoring system
JP2001323828A (en) * 2000-05-16 2001-11-22 Nissan Motor Co Ltd Compression self-ignition gasoline engine
US6466858B1 (en) * 2000-11-02 2002-10-15 General Electric Company Methods and apparatus for monitoring gas turbine engine operation
US6845306B2 (en) 2000-11-09 2005-01-18 Honeywell International Inc. System and method for performance monitoring of operational equipment used with machines
JP3979081B2 (en) * 2001-01-16 2007-09-19 日産自動車株式会社 Combustion control system for internal combustion engine
US6671589B2 (en) 2001-02-13 2003-12-30 William Holst Method and apparatus to support remote and automatically initiated data loading and data acquisition of airborne computers using a wireless spread spectrum aircraft data services link
US6643569B2 (en) 2001-03-30 2003-11-04 The Regents Of The University Of Michigan Method and system for detecting a failure or performance degradation in a dynamic system such as a flight vehicle
US6741938B2 (en) 2001-10-30 2004-05-25 Delphi Technologies, Inc. Method for continuously predicting remaining engine oil life
US20030093211A1 (en) * 2001-11-15 2003-05-15 Zagranski Raymond D. Method of engine surge discrimination
DE60230791D1 (en) * 2001-11-15 2009-02-26 Goodrich Pump & Engine Control METHOD AND DEVICE FOR AVOIDING THE PUMP IN A GAS TURBINE
US6748325B1 (en) * 2001-12-07 2004-06-08 Iwao Fujisaki Navigation system
US6789000B1 (en) * 2002-04-16 2004-09-07 Altek Power Corporation Microprocessor-based control system for gas turbine electric powerplant
US6935120B2 (en) * 2002-05-09 2005-08-30 General Electric Company Approach to extending life of gas turbine engine
US7505604B2 (en) * 2002-05-20 2009-03-17 Simmonds Precision Prodcuts, Inc. Method for detection and recognition of fog presence within an aircraft compartment using video images
JP3684208B2 (en) * 2002-05-20 2005-08-17 株式会社東芝 Gas turbine control device
GB0211644D0 (en) * 2002-05-21 2002-07-03 Wesby Philip B System and method for remote asset management
US6865890B2 (en) 2002-06-07 2005-03-15 Ronald Steven Walker Software system for verification of gas fuel flow
JP2004108291A (en) * 2002-09-19 2004-04-08 Ishikawajima Harima Heavy Ind Co Ltd Part deterioration prediction method and performance deterioration prediction method for gas turbine engine
US6741203B1 (en) * 2002-10-28 2004-05-25 Rockwell Collins Adaptive radar thresholds system and method
US6823675B2 (en) * 2002-11-13 2004-11-30 General Electric Company Adaptive model-based control systems and methods for controlling a gas turbine
US6892127B2 (en) * 2003-02-28 2005-05-10 General Electric Company Methods and apparatus for assessing gas turbine engine damage
US20040244633A1 (en) * 2003-05-08 2004-12-09 Witmer Warner H. Cats-constrained airplane transportation system
DE10337372B4 (en) * 2003-08-13 2005-08-04 Airbus Deutschland Gmbh Device for stabilizing the engine inlet flow in engine stands
US7246002B2 (en) * 2003-11-20 2007-07-17 General Electric Company Method for controlling fuel splits to gas turbine combustor
US7129857B1 (en) * 2004-02-26 2006-10-31 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Intelligent weather agent
US7487029B2 (en) * 2004-05-21 2009-02-03 Pratt & Whitney Canada Method of monitoring gas turbine engine operation
US7307549B2 (en) * 2005-07-05 2007-12-11 Gulfstream Aerospace Corporation Standby display aircraft management system

Also Published As

Publication number Publication date
US20050261820A1 (en) 2005-11-24
JP2007538234A (en) 2007-12-27
EP1747446A1 (en) 2007-01-31
US20090229272A1 (en) 2009-09-17
US7487029B2 (en) 2009-02-03
CA2565147C (en) 2009-10-13
WO2005114129A1 (en) 2005-12-01
US8594903B2 (en) 2013-11-26
EP1747446A4 (en) 2010-03-03

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